Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface

Yu Jiang; Kai Zheng; Baoqing Yang

doi:10.1109/ChiCC.2014.6896593

Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface

Yu Jiang^*
, Kai Zheng
, Baoqing Yang

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology
Dalian Maritime University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In this paper we investigate the attitude control problems of underactuated spacecraft by moving masses. First, the attitude dynamics and kinematics equations of underactuated spacecrafts with two moving masses are given. Then, considering the stabilization of the roll and pitch attitude, We present a controller designed using a linear Lipschtiz surface combined with the traditional sliding model control method. This method can increase the parameters degree of freedom to solve the control problem brought by the constraints of underactuated system. Using the contingent cone criteria, the existence and accessibility conditions of the switching surface are addressed. Eventually, based on the equivalence principle, the controllers for the roll, pitch and yaw attitude stabilization are presented and testified by the simulation, respectively. The simulation results show the effectiveness of the proposed method.

Original language	English
Title of host publication	Proceedings of the 33rd Chinese Control Conference, CCC 2014
Editors	Shengyuan Xu, Qianchuan Zhao
Publisher	IEEE Computer Society
Pages	43-48
Number of pages	6
ISBN (Electronic)	9789881563842
DOIs	https://doi.org/10.1109/ChiCC.2014.6896593
State	Published - 11 Sep 2014
Externally published	Yes
Event	Proceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China Duration: 28 Jul 2014 → 30 Jul 2014

Publication series

Name	Proceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	Proceedings of the 33rd Chinese Control Conference, CCC 2014
Country/Territory	China
City	Nanjing
Period	28/07/14 → 30/07/14

Keywords

Mass Moment Spacecraft
Nonsmooth Switching Surface
Underactuated Control
Variable Structure Control

Access to Document

10.1109/ChiCC.2014.6896593

Cite this

Jiang, Y., Zheng, K., & Yang, B. (2014). Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface. In S. Xu, & Q. Zhao (Eds.), Proceedings of the 33rd Chinese Control Conference, CCC 2014 (pp. 43-48). Article 6896593 (Proceedings of the 33rd Chinese Control Conference, CCC 2014). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2014.6896593

@inproceedings{a251218b3e4e4ee9aac898f9959318e4,

title = "Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface",

abstract = "In this paper we investigate the attitude control problems of underactuated spacecraft by moving masses. First, the attitude dynamics and kinematics equations of underactuated spacecrafts with two moving masses are given. Then, considering the stabilization of the roll and pitch attitude, We present a controller designed using a linear Lipschtiz surface combined with the traditional sliding model control method. This method can increase the parameters degree of freedom to solve the control problem brought by the constraints of underactuated system. Using the contingent cone criteria, the existence and accessibility conditions of the switching surface are addressed. Eventually, based on the equivalence principle, the controllers for the roll, pitch and yaw attitude stabilization are presented and testified by the simulation, respectively. The simulation results show the effectiveness of the proposed method.",

keywords = "Mass Moment Spacecraft, Nonsmooth Switching Surface, Underactuated Control, Variable Structure Control",

author = "Yu Jiang and Kai Zheng and Baoqing Yang",

note = "Publisher Copyright: {\textcopyright} 2014 TCCT, CAA.; Proceedings of the 33rd Chinese Control Conference, CCC 2014 ; Conference date: 28-07-2014 Through 30-07-2014",

year = "2014",

month = sep,

day = "11",

doi = "10.1109/ChiCC.2014.6896593",

language = "英语",

series = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",

publisher = "IEEE Computer Society",

pages = "43--48",

editor = "Shengyuan Xu and Qianchuan Zhao",

booktitle = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",

address = "美国",

}

Jiang, Y, Zheng, K & Yang, B 2014, Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface. in S Xu & Q Zhao (eds), Proceedings of the 33rd Chinese Control Conference, CCC 2014., 6896593, Proceedings of the 33rd Chinese Control Conference, CCC 2014, IEEE Computer Society, pp. 43-48, Proceedings of the 33rd Chinese Control Conference, CCC 2014, Nanjing, China, 28/07/14. https://doi.org/10.1109/ChiCC.2014.6896593

Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface. / Jiang, Yu; Zheng, Kai; Yang, Baoqing.
Proceedings of the 33rd Chinese Control Conference, CCC 2014. ed. / Shengyuan Xu; Qianchuan Zhao. IEEE Computer Society, 2014. p. 43-48 6896593 (Proceedings of the 33rd Chinese Control Conference, CCC 2014).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface

AU - Jiang, Yu

AU - Zheng, Kai

AU - Yang, Baoqing

PY - 2014/9/11

Y1 - 2014/9/11

N2 - In this paper we investigate the attitude control problems of underactuated spacecraft by moving masses. First, the attitude dynamics and kinematics equations of underactuated spacecrafts with two moving masses are given. Then, considering the stabilization of the roll and pitch attitude, We present a controller designed using a linear Lipschtiz surface combined with the traditional sliding model control method. This method can increase the parameters degree of freedom to solve the control problem brought by the constraints of underactuated system. Using the contingent cone criteria, the existence and accessibility conditions of the switching surface are addressed. Eventually, based on the equivalence principle, the controllers for the roll, pitch and yaw attitude stabilization are presented and testified by the simulation, respectively. The simulation results show the effectiveness of the proposed method.

AB - In this paper we investigate the attitude control problems of underactuated spacecraft by moving masses. First, the attitude dynamics and kinematics equations of underactuated spacecrafts with two moving masses are given. Then, considering the stabilization of the roll and pitch attitude, We present a controller designed using a linear Lipschtiz surface combined with the traditional sliding model control method. This method can increase the parameters degree of freedom to solve the control problem brought by the constraints of underactuated system. Using the contingent cone criteria, the existence and accessibility conditions of the switching surface are addressed. Eventually, based on the equivalence principle, the controllers for the roll, pitch and yaw attitude stabilization are presented and testified by the simulation, respectively. The simulation results show the effectiveness of the proposed method.

KW - Mass Moment Spacecraft

KW - Nonsmooth Switching Surface

KW - Underactuated Control

KW - Variable Structure Control

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M3 - 会议稿件

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BT - Proceedings of the 33rd Chinese Control Conference, CCC 2014

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Y2 - 28 July 2014 through 30 July 2014

ER -

Attitude control design of underactuated mass moment spacecraft based on nonsmooth Lipschitz surface

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